# Service difficulty reports: N602TW, cancelled Apr 2, 2003 A list on [N602TW, cancelled Apr 2, 2003](https://openairdocs.org/deregistered/N602TW-2003-04-02.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 72 reports - [SDR TWAA0103101](https://openairdocs.org/sdr/TWAA0103101.md): Power Supply · discharged · Feb 16, 2001 · N602TW · Boeing 767231 · Emergency Lighting > THE EGRESS LIGHTS ON RT SIDE OF CABIN ROWS 11 THRU 16 ILLUMINATED INTERMITTENTLY. REPLACED THE POWER SUPPLY. CHECK-C 11-29-00 LAX. - [SDR TWAA0018902](https://openairdocs.org/sdr/TWAA0018902.md): Flap · punctured · Dec 5, 2000 · N602TW · Boeing 767231 · Trailing Edge Flaps > DURING CHECK-C MAINT ON RT WING FOUND 2 PUNCTURES INSIDE FLAP UNDER PANEL 666NT. FILLED HOLES WITH 934 ADHESIVE. ACCOMPLISHED HOT BOND METAL TO METAL REPAIR PER SRM 51-70-10, PAGE 30. - [SDR TWAA0018906](https://openairdocs.org/sdr/TWAA0018906.md): Skin · delaminated · Dec 4, 2000 · N602TW · Boeing 767231 · Trailing Edge Flaps > DURING CHECK-C MAINT THE RT WING INBD FLAP HAD DELAMINATION ON COMPOSITE MATERIAL AT APPROX. 45 INCHES, 55 INCHES, AND 60 INCHES FROM INBD SIDE. REMOVED SKIN AND INSTALLED HOT BOND REPAIRS TO COVER ALL 3 AREAS, PER SRM 51-70-05. - [SDR TWAA0018903](https://openairdocs.org/sdr/TWAA0018903.md): Skin · delaminated · Dec 4, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT FOUND NUMBER 8 L/E SLAT INBD EDGE WAS DELAMINATED ON PREVIOUS REPAIR IN TWO PLACES, ONE EA INSIDE (BACK) AND OUTER SKIN. INSTALLED A 11 IN BY 5 IN METAL BOND REPAIR PER SRM 51-70-10. - [SDR TWAA0018905](https://openairdocs.org/sdr/TWAA0018905.md): Doubler · delaminated · Dec 3, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT THE LT WING NUMBER 3 L.E. SLAT REPAIR, INBD EDGE WAS NOT ADHEARING TO SKIN. REMOVED OLD REPAIR AND INSTALLED NEW 6 IN BY 6 IN METAL TO METAL REPAIR PER SRM 51-70-00. - [SDR TWAA0018904](https://openairdocs.org/sdr/TWAA0018904.md): Doubler · delaminated · Nov 30, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT THE NUMBER 7 L/E SLAT HAD 4 BY 5 PREVIOUS REPAIR THAT HAD DELAMINATION IN CENTER OF REPAIR. INSTALLED A 4 1/2 BY 7 IN METAL BOND REPAIR PER SRM 51-70-10. - [SDR TWAA0018503](https://openairdocs.org/sdr/TWAA0018503.md): Power Supply · worn · Nov 27, 2000 · N602TW · Boeing 767231 · Emergency Lighting > THE EGRESS LIGHTS ON THE LEFT SIDE OF THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 8-1-00 LAX. - [SDR TWAA0018101](https://openairdocs.org/sdr/TWAA0018101.md): Power Supply · inoperative · Nov 17, 2000 · N602TW · Boeing 767231 · Emergency Lighting > THE FIRST CLASS SECTION EGRESS LIGHTS WERE INOPERATIVE ON LT SIDE OF CABIN. REPLACED THE BATTERY PACK. CHECK-C 8-1-00 LAX. - [SDR TWAA0016701](https://openairdocs.org/sdr/TWAA0016701.md): Battery Pack · discharged · Oct 26, 2000 · N602TW · Boeing 767231 · Emergency Lighting > THE EGRESS LIGHT ON LT SIDE OF FIRST CLASS, AND THE FWD GALLEY CROSS WALK EGRESS LIGHTS, WERE INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS MALFUNCTION, AND REPAIRED JUMPER CABLE FOR THE GALLEY CROSS WALK. CHECK-C 8-1-00 LAX. - [SDR TWAA0006434](https://openairdocs.org/sdr/TWAA0006434.md): Skin · debonded · Apr 24, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT, THE LT WING NUMBER 6 LEADING EDGE SLAT TOP SIDE AT MID SPAN HAD THE HOT BOND LIFTED AND HAD BEEN SEALED WITH SPEED TAPE PER SRM 57-43-02. APPLIED HOT BOND REPAIR ON NUMBER 6 SLAT APPROX 3.75 BY 4.75 INCH DOUBLER PER SRM 57-43-20 AND 51- - [SDR TWAA0006433](https://openairdocs.org/sdr/TWAA0006433.md): Skin · dented · Apr 24, 2000 · N602TW · Boeing 767231 · Trailing Edge Flaps > DURING CHECK-C MAINT, THE RT WING LEADING EDGE OF I/B TRAILING EDGE FLAP HAD A 1 INCH DENT, 2 FT I/B FROM THE O/B END. APPLIED FILLER ADHESIVE ON TRAILING EDGE FLAP PER SRM 57-53-01, PAGE 101. SANDED, PRIMED AND PAINTED PER SPM 1-20-02. - [SDR TWAA0006302](https://openairdocs.org/sdr/TWAA0006302.md): Skin · delaminated · Apr 19, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT, THE LT WING NUMBER 2 L/E SLAT O/B END, THE T/E WEDGE HAD A BULGE THAT WAS DELAMINATING. APPLIED HOT BOND REPAIR ON NR 2 SLAT APPROX 4 IN BY 3.5 DOUBLER PER SRM 57-43-02 AND 51-70-10. - [SDR TWAA0006301](https://openairdocs.org/sdr/TWAA0006301.md): Structure · damaged · Apr 19, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT, THE LT WING NUMBER 4 L/E SLAT ASSY HAD A HOLE IN THE INSIDE SURFACE. FILLED DAMAGED AREA AND APPLIED 2 IN BY 2 IN METAL TO METAL HOT BOND. PRIMED AND PAINTED PER SRM 51-70-10. - [SDR TWAA0006206](https://openairdocs.org/sdr/TWAA0006206.md): Skin · delaminated · Apr 19, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT THE RH WING NUMBER 10 L/E SLAT HAD 5 INCH SQUARE DOUBLER THAT WAS DELAMINATING, ON TOP SURFACE, 5 FT I/B FROM THE O/B END. REMOVED DELAMINATED PATCH. CLEANED AREA, FABRICATED NEW DOUBLER 5 INCH BY 6 INCH AND HOT BOND PER SRM 51-70-10. S - [SDR TWAA0006205](https://openairdocs.org/sdr/TWAA0006205.md): Skin · delaminated · Apr 19, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINT, FOUND RT WING NUMBER 7 L/E SLAT REPAIR HAD A 6 INCH BY 4 INCH DELAMINATION, 4 INCHES FROM THE I/B END, ON TOP. APPLIED HOT BOND REPAIR ON NUMBER 7 SLAT, APPROX 5.5 INCH BY 5.5 INCH DOUBLER PER SRM 57-43-02 AND 51-70-10. SEALED EDGES PER - [SDR TWAA0002001](https://openairdocs.org/sdr/TWAA0002001.md): Skin · delaminated · Feb 3, 2000 · N602TW · Boeing 767231 · Leading Edge Devices > DURING CHECK-C MAINTENANCE, THE NUMBER 1 LE SLAT TOP SIDE, AN EXISTING 6 IN BY 6 IN PATCH WAS LOOSE AND DELAMINATING AT THE INBD TE WEDGE. REMOVED OLD REPAIR. INSTALLED METAL TO METAL 250 DEGREEE HOT BOND REPAIR PER SRM 51-70-10 AND SRM 57-43-02. - [SDR TWAA9914601](https://openairdocs.org/sdr/TWAA9914601.md): Battery · discharged · Oct 29, 1999 · N602TW · Boeing 767231 · Emergency Lighting > DURING PREFLIGHT, FOUND EGRESS LIGHTS INOP FROM SEAT 33 LT TO ROW 35 LT. REPLACED BATTERY. CC 10-24-99 LAX. - [SDR TWAA9913904](https://openairdocs.org/sdr/TWAA9913904.md): Switch · failed · Oct 10, 1999 · N602TW · Boeing 767231 · Engine Oil Indicating System > IN AN ETOPS FLIGHT SEGMENT THE LEFT ENGINE FILTER BYPASS LIGHT BLINKED THEN CAME ON STEADY. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO TER. THE MAIN OIL SCREEN AND CHIP DETECTORS WERE CLEAN. PLACARD THE FILTER BYPASS LIGHT INOPERATIVE PER MEL AND T - [SDR TWAA9913302](https://openairdocs.org/sdr/TWAA9913302.md): Light · damaged · Sep 28, 1999 · N602TW · Boeing 767231 · Emergency Lighting > FOUND CABIN EGRESS LIGHTS INOPERATIVE AT THE NUMBER 2 CROSSOVER POINT. REPLACED THE LIGHT STRIP. CHECK-C 8-25-99 LAX. - [SDR TWAA9908006](https://openairdocs.org/sdr/TWAA9908006.md): Tee · worn · Jun 2, 1999 · N602TW · Boeing 767231 · Elevator Structure > DURING CHECK-C MAINT MO 72F01 CALLED FOR REPLACING THE RT ELEVATOR SLAVE LINKAGE LOST MOTION DEVICE TEE. REPLACED TEE PER SERVICE BULLETIN 27A0136, REV 1. - [SDR TWAA9907202](https://openairdocs.org/sdr/TWAA9907202.md): Bulb · failed · May 14, 1999 · N602TW · Boeing 767231 · Emergency Lighting > FOUND EXTERNAL EMERGENCY LIGHT INOPERATIVE AT THE NUMBER 4 DOOR ON LT SIDE OF FUSELAGE. REPLACED THE BULB. CHECK-C 2-26-99 LAX. - [SDR TWAA9907201](https://openairdocs.org/sdr/TWAA9907201.md): Bulb · failed · May 14, 1999 · N602TW · Boeing 767231 · Emergency Lighting > THE AFT GALLEY CEILING EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 2-26-99 LAX. - [SDR TWAA9906103](https://openairdocs.org/sdr/TWAA9906103.md): Skin · delaminated · Apr 25, 1999 · N602TW · Boeing 767231 · Leading Edge Devices > THE NR 7 LEADING EDGE SLAT TRAILING EDGE WEDGE HAD DELAMINATION APPROX 8.5 FT FROM I/B EDGE. AREAS APPROX 2.5 INCHES IN DIAMETER AND 1.5 INCH APART ON LOWER SURFACE, 2.5 INCHES FROM THE TRAILING EDGE. INSTALLED PERMANENT REPAIR PER SRM 51-70-10, WITH CORE AN - [SDR TWAA9901701](https://openairdocs.org/sdr/TWAA9901701.md): Power Supply · inop · Jan 19, 1999 · N602TW · Boeing 767231 · Emergency Lighting > FOUND FLOOR EGRESS LIGHTS OUT ON LT SIDE OF CABIN FROM ROW 24 TO ROW 33. REPLACED POWER SUPPLY. CHECK-C 11-17-98 MCI. - [SDR TWAA9818311](https://openairdocs.org/sdr/TWAA9818311.md): Stringer · corroded · Nov 6, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R CORRODED BETWEEN STA 610 AND 632. REMOVED S39R AT STA 600 TO 622 AND INSTALLED NEW FABRICATED PART PER SRM 53-00-03. - [SDR TWAA9901008](https://openairdocs.org/sdr/TWAA9901008.md): Skin · corroded · Oct 30, 1998 · N602TW · Boeing 767231 · Fuselage Main, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND STA 1269, STRINGER 39R WITH CORROSION BETWEEN INBD SIDE OF STRINGER AND FUSELAGE SKIN, AND STRINGER 39L CORRODED BETWEEN STRINGER AND SKIN AT STA 1264. CUT OUT SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR PER ARA 15766 AND SRM 5 - [SDR TWAA9818206](https://openairdocs.org/sdr/TWAA9818206.md): Stringer · corroded · Oct 30, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND CORROSION ON LOWER SIDE OF STRINGER 38R, STA 565. CUT OUT CORROSION PER SRM 51-10-03 PAGE 16. INSTALLED SECTION OF STRINGER AT 38R STA 565 PER SRM 53-00-03, FIG 202. - [SDR TWAA9818205](https://openairdocs.org/sdr/TWAA9818205.md): Stringer · corroded · Oct 30, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 39L BETWEEN STA 616 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632 PER SRM 51-10-00 PAGE 16. INSTALLED SPLICE BETWEEN STA 600 TO 632 PER SRM 53-00-03, PAGE 215 DETAIL III FIG 207 - [SDR TWAA9818204](https://openairdocs.org/sdr/TWAA9818204.md): Stringer · corroded · Oct 30, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND CORRODED STRINGER 38R BETWEEN STA 610 TO 632. CUT OUT SECTION OF STRINGER FROM STA 600 TO 627. REMOVED CORROSION PER SRM 51-10-00 PAGE 16. INSTALLED CRACK REPAIR PER SRM 53-00-03 PAGE 219 FIG 203 SHEET 3. - [SDR TWAA9818203](https://openairdocs.org/sdr/TWAA9818203.md): Stringer · corroded · Oct 30, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND STRINGER 39L CORRODED AT STA 610 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632. INSTALLED SPLICE BETWEEN STA 600 TO 637 PER SRM 53-00-03, PAGE 215 DETAIL 14, FIG 207 SHEET A. - [SDR TWAA9818202](https://openairdocs.org/sdr/TWAA9818202.md): Stringer · corroded · Oct 29, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND CORROSION AT STA 580 STRINGER 39L ON THE STRINGER. SPLICED STRINGER AT STA 577 TO 600 PER SRM 53-00-03 PAGE 215, DETAIL III, FIG 207. - [SDR TWAA9818302](https://openairdocs.org/sdr/TWAA9818302.md): Stringer · corroded · Oct 26, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND STRINGER 39R WITH EXFOLIATION CORROSION AT STA 561 TO 562, ON TOP INBD LIP APPROX 1 IN LONG. CORROSION REMOVED AND REPAIRED WITH J-ANGLE PER SRM 53-00-03, PAGE 218. - [SDR TWAA9818012](https://openairdocs.org/sdr/TWAA9818012.md): Skin · corroded · Oct 26, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, CENTER WING UPPER SKIN WAS CUT OUT FOR CORROSION TO SKIN STA 853 TO 855. RECTANGULAR SECT FRONT 71 RBL TO 84 RBL AND REAR 69 RBL TO 86 RBL. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER 51-00-03 PART 6 OF TWA NDT MANUAL AND NO - [SDR TWAA9818011](https://openairdocs.org/sdr/TWAA9818011.md): Skin · corroded · Oct 26, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND BELOW UPPER CENTER WING SKIN SUPPORT BEAM WITH EXIFOLIATION CORROSION THRU BEAM. CORROSION VISIBLE FROM STA 855 TO 853 RBL 75 TO RBL 86. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-10-03, PART 6 AND - [SDR TWAA9818010](https://openairdocs.org/sdr/TWAA9818010.md): Skin · corroded · Oct 26, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND INTERGRANULAR CORROSION ON CENTER UPPER WING SKIN AT STA 954.5 TO 858, RBL 75 TO RBL 88. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION AND APPLIED R - [SDR TWAA9818009](https://openairdocs.org/sdr/TWAA9818009.md): Skin · corroded · Oct 26, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION AT STA 860 BELOW EMERGENCY EXIT ON RT SIDE. CUT OUT CORRODED AREA PER SRM 51-10-00. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 AND NO CRACKS FOUND. REMOVED C - [SDR TWAA9818008](https://openairdocs.org/sdr/TWAA9818008.md): Skin · corroded · Oct 26, 1998 · N602TW · Boeing 767231 · Fuselage Main, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION AT UPPER SKIN STA 830 TO 852, RBL 74 TO RBL 97. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDY CURRENT PER 51-10-03, PART 6 AND NO CRACKS FOUND. REPAIRED PER TWA ARA 11596. - [SDR TWAA9818210](https://openairdocs.org/sdr/TWAA9818210.md): Stringer · cracked · Oct 22, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PAGE 209 FIG 202. - [SDR TWAA9818209](https://openairdocs.org/sdr/TWAA9818209.md): Stringer · cracked · Oct 22, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND FWD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1. - [SDR TWAA9818208](https://openairdocs.org/sdr/TWAA9818208.md): Stringer · cracked · Oct 22, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PG 209 FIG 202. - [SDR TWAA9818207](https://openairdocs.org/sdr/TWAA9818207.md): Stringer · corroded · Oct 22, 1998 · N602TW · Boeing 767231 · Fuselage Main, Longeron/Stringer > DURING OP 15 MAINT CHECK, FOUND FORWARD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1. - [SDR TWAA9818312](https://openairdocs.org/sdr/TWAA9818312.md): Skin · gouged · Oct 21, 1998 · N602TW · Boeing 767231 · Elevator, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND LT ELEV HAD ONE INCH LONG GOUGE IN UPPER SURPACE, 29 IN OTBD FROM OTBD ACTUATOR, AND 15 IN AFT FROM THE LEADING EDGE. REMOVED DAMAGED AREA AND REPAIRED WITH 6 PLIES OF GRAPHITE OVERLAY PER SRM 55-20-01, PAR 3C, AND 51-10-17, PA - [SDR TWAA9818007](https://openairdocs.org/sdr/TWAA9818007.md): Skin · corroded · Oct 19, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND CORROSION AT UPPER SKIN CENTER WING AT STA 850 TO 852.5, RBL 83.5 TO RBL 88.5, INTERGRANULAR CORROSION. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. ACCOMP HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6 AND NO CRACKS FO - [SDR TWAA9818006](https://openairdocs.org/sdr/TWAA9818006.md): Skin · corroded · Oct 19, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND CORROSION ON CENTER FUEL TANK UPPER SKIN AT STA 846, RBL 79 TO 83. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. NO CRACKS FOUND USING HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6. REPAIRED PER ARA 11596. - [SDR TWAA9817806](https://openairdocs.org/sdr/TWAA9817806.md): Skin · corroded · Oct 16, 1998 · N602TW · Boeing 767231 · Fuselage Main, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SKIN, STA 830 TO 852, LBL 74 IN TO LBL 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS FOUND. REPAIRED PER ARA 11596. - [SDR TWAA9817805](https://openairdocs.org/sdr/TWAA9817805.md): Skin · corroded · Oct 16, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION, STA 860 BELOW EMERGENCY EXIT ON LT SIDE. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REPAIRED PER ARA 1159 - [SDR TWAA9817804](https://openairdocs.org/sdr/TWAA9817804.md): Skin · corroded · Oct 16, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING AT FASTENERS STA 883 TO 911, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION PER SRM 51-10-11. REPAIRED PER ARA 11596. - [SDR TWAA9817803](https://openairdocs.org/sdr/TWAA9817803.md): Skin · corroded · Oct 16, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND CORROSION AT TOP WING SKIN AT FASTENERS STA 911 TO 933, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS WERE FOUND. REMOVED CORROSION PER SRM 51-10-00. SPOT FACED AND BLENDED AS NEEDED - [SDR TWAA9817802](https://openairdocs.org/sdr/TWAA9817802.md): Skin · corroded · Oct 16, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 933 TO 965, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT EDDY CURRENT PER 51-00-03 PART 5, FOUND NO CRACKS. SPOT FACED AND BLENDED AS NEEDED PER MCI 98-0185RE. REPAI - [SDR TWAA9817801](https://openairdocs.org/sdr/TWAA9817801.md): Skin · corroded · Oct 16, 1998 · N602TW · Boeing 767231 · Wing, Plate/Skin > DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 859 TO 883, LBL 74 IN TO 97 IN. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT OF HOLES PER 51-00-03, PART 6, FOUND NO CRACKS. REPAIRED PER ARA 11596. Next page: https://openairdocs.org/deregistered/N602TW-2003-04-02/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N602TW' AND deregistration_id = 'N602TW-2003-04-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N602TW-2003-04-02/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.